2840-00-955-1489

Aircraft Gas Turbine Engine Combustion Chamber

2840009551489 009551489

The portion of an ENGINE, GAS TURBINE, AIRCRAFT in which fuel is burned. It may be an annular type in which the space between the circular inner and outer cylinders form the burning chamber or it may be the multi-arrangement can type in which separate can like burn cylinders are positioned in a circular arrangement within an inner and outer case. View more Aircraft Gas Turbine Engine Combustion Chamber

2840-00-955-1489 CHAMBER,COMBUSTION,AIRCRAFT GAS TURBINE ENGINE 2840009551489 009551489

Managed by United States
NSN Created on 9 May 1966
Data Last Changed
November 2023
NATO Update Count
7
NATO Data Quality
2840-00-955-1489 CHAMBER,COMBUSTION,AIRCRAFT GAS TURBINE ENGINE 2840009551489 009551489 1/1
NSN 2840-00-955-1489 (Generic Image) 1/1

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2840-00-955-1489 Demil Restrictions 2840-00-955-1489

DEMIL: B | DEMILI: | CRITICALITY: Y | HMIC: N | PMIC: A | EDC: | ADPEC:

2840-00-955-1489 is a Aircraft Gas Turbine Engine Combustion Chamber that does not have a nuclear hardened feature, but does have another critical feature or features such as tolerance, fit restriction or application. This item is a US Munitions List Item and must be mutilated to scrap. This item is not suspected to be hazardous. This item does not contain a precious metal.

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